Airfoil database search

Search the 1638 airfoils available in the databases filtering by name, thickness and camber. Click on an airfoil image to display a larger preview picture. There are links to the original airfoil source and dat file and the details page with polar diagrams for a range of Reynolds numbers.

(goe462-il) GOE 462 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 462 airfoil Max thickness 11% at 9.9% chord Max camber 13.4% at 29.9% chord Source UIUC Airfoil Coordinates Database
(goe464-il) GOE 464 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 464 airfoil Max thickness 7.7% at 7.4% chord Max camber 9.9% at 29.9% chord Source UIUC Airfoil Coordinates Database
(goe474-il) GOE 474 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 474 airfoil Max thickness 7% at 30% chord Max camber 2.9% at 40% chord Source UIUC Airfoil Coordinates Database
(goe476-il) GOE 476 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 476 airfoil Max thickness 14.5% at 29.5% chord Max camber 5.2% at 39.5% chord Source UIUC Airfoil Coordinates Database
(goe477-il) GOE 477 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 477 airfoil Max thickness 10.1% at 30% chord Max camber 4.9% at 40% chord Source UIUC Airfoil Coordinates Database
(goe478-il) GOE 478 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 478 airfoil Max thickness 13.4% at 29.6% chord Max camber 4.3% at 39.6% chord Source UIUC Airfoil Coordinates Database
(goe479-il) GOE 479 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 479 airfoil Max thickness 11.6% at 30% chord Max camber 4% at 40% chord Source UIUC Airfoil Coordinates Database
(goe480-il) GOE 480 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 480 airfoil Max thickness 11.8% at 30% chord Max camber 5.5% at 40% chord Source UIUC Airfoil Coordinates Database
(goe481-il) GOE 481 AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 481 airfoil Max thickness 13.4% at 9.6% chord Max camber 8.8% at 39.4% chord Source UIUC Airfoil Coordinates Database
(goe481a-il) GOE 481A AIRFOIL		Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file
	Gottingen 481A airfoil Max thickness 15.3% at 29.4% chord Max camber 5.5% at 39.4% chord Source UIUC Airfoil Coordinates Database

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